Inventor

LAFONT LAURENT

FR39 patents

⚠️ This page may combine multiple inventors who share the name “LAFONT LAURENT”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.

LAFONT LAURENT

AIRBUS OPERATIONS SAS

Vane for aircraft turbine engine receiver, provided with two hollow cores lodged in one another

Assembly for aircraft comprising a wing system element as well as an attachment mast

Engine assembly for aircraft

Assembly for aircraft comprising a primary structure of an attachment pylon attached to a wing box using a bolted connection

Rear part of an aircraft comprising a structure for supporting engines, extending through the fuselage and connected thereto by at least one connecting rod

Propulsion assembly comprising a fuel conditioning system positioned behind a debris ejection zone, aircraft comprising at least one such propulsion assembly

Assembly for aircraft comprising a primary mounting pylon structure fixed to an airfoil box using a bolted link

Device for measuring a pattern of forces and moments generated by an aircraft propulsion system

Propulsion assembly for an aircraft, comprising a load support

Propulsion unit with propeller and electric motor comprising an adapted primary structure, and aircraft having at least one such propulsion unit

Pylon including a primary structure formed of at least one longeron and one panel assembled by welding

Computing unit assembly and a method and a system for synchronizing computing units of an aircraft

Aircraft engine assembly, comprising an engine attachment device equipped with structural movable cowls connected to the central box

LAFONT LAURENT

Blade-retaining device for turbomachine propeller

Blade retaining device for turbo machine propeller

Engine assembly for an aircraft the engine attachment strut of which includes a structural case forming an internal radial delimitation of the secondary flow

Take-up device for thrust forces with connecting rods for aircraft engine attachment pylon, integrating three aligned ball joints

Propeller for an aircraft turbine engine comprising a vane retaining ring mounted about the hub

Assembly for an aircraft comprising a turbomachine attachment strut of which the means for attachment to the wing are arranged in a T shape

Rear part of an aircraft comprising a structure for supporting engines, extending through the fuselage and connected thereto by at least one connecting rod

Aircraft engine attachment pylon comprising two front wing system attachments with orthogonal shearing pins

Method for mounting an aircraft engine on a rigid structure of a strut for locking the engine

Rear part of an aircraft including an engine support structure assembled so as to oscillate on the fuselage

Rear part of an aircraft comprising a structure for supporting engines, connected to the fuselage by at least one blocking element under compression loading

AIRBUS FRANCE

Mounting assembly for securing an engine to an aircraft wing

Engine assembly for aircraft

Strut for locking the engine of an aircraft

Engine mounting structure for an aircraft

Engine mounting structure for an aircraft

Engine suspension pylon for aircraft

Assembly for an aircraft including a wing element and a suspension pylon

Engine mounting structure interposed between an aircraft wing system and said engine

JOURNADE FREDERIC

Engine assembly for aircraft with sliding nacelle

Aircraft assembly including an element for mounting an engine and associated aircraft

Aircraft engine mounting structure, assembly comprising this structure and associated aircraft

JOURNADE FRÉDÉRIC

Engine assembly for an aircraft comprising attachments for engines offset below on the fan frame

BONNET MATHIEU

Structural rod incorporating a vibration filtration mode

COMBES STEPHANE

System for connecting a crossbar to an aircraft engine pylon

DIOCHON LIONEL

Turbojet engine mounting structure for aircraft